20211119019669A

Accident · Substantial damage

FAA accident report · Robinson Helicopter R22 BETA · Miamisburgh, OH · November 19, 2021

Date
November 19, 2021 · 11:30 local
Place
Miamisburgh, OH
Phase of flight
Taxi
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N221HG
NTSB investigation
NTSBCEN22LA041
Reported as
Robinson Helicopter R22 Beta
Reported engine
Lycoming 0-320 series
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Student
Pilot’s flight hours
48 total48 in this make and model22 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

On 11/19/2021, the student pilot operating N221HG during solo operations had a loss of control after lifting the aircraft off the ramp area. The pilot attempted to counteract the torque by applying pedal control. The pilot's input was excessive and required opposite control, which was also excessive. At this point, the pilot attempted to correct by reducing the collective, but this action was not sufficient to stop the oscillations and the helicopter began to rotate out of his control. The helicopter rotated around 360 degrees, and struck the tail on the ramp breaking off the tail rotor. The helicopter dropped back to the ramp with enough force to break the skids support.

As the FAA filed it

ON 11/19/2021, THE STUDENT PILOT OPERATING N221HG DURING SOLO OPERATIONS HAD A LOSS OF CONTROL AFTER LIFTING THE AIRCRAFT OFF THE RAMP AREA. THE PILOT ATTEMPTED TO COUNTERACT THE TORQUE BY APPLYING PEDAL CONTROL. THE PILOT'S INPUT WAS EXCESSIVE AND REQUIRED OPPOSITE CONTROL, WHICH WAS ALSO EXCESSIVE. AT THIS POINT, THE PILOT ATTEMPTED TO CORRECT BY REDUCING THE COLLECTIVE, BUT THIS ACTION WAS NOT SUFFICIENT TO STOP THE OSCILLATIONS AND THE HELICOPTER BEGAN TO ROTATE OUT OF HIS CONTROL. THE HELICOPTER ROTATED AROUND 360 DEGREES, AND STRUCK THE TAIL ON THE RAMP BREAKING OFF THE TAIL ROTOR. THE HELICOPTER DROPPED BACK TO THE RAMP WITH ENOUGH FORCE TO BREAK THE SKIDS SUPPORT.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.